CN219829205U - Forming die for aerospace component - Google Patents

Forming die for aerospace component Download PDF

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Publication number
CN219829205U
CN219829205U CN202321178613.5U CN202321178613U CN219829205U CN 219829205 U CN219829205 U CN 219829205U CN 202321178613 U CN202321178613 U CN 202321178613U CN 219829205 U CN219829205 U CN 219829205U
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China
Prior art keywords
fixedly connected
joint
cooling tube
forming die
base
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CN202321178613.5U
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Chinese (zh)
Inventor
黎宇航
赵玉琼
曹春晓
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Nanjing Zebai High End Equipment Co ltd
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Nanjing Zebai High End Equipment Co ltd
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Abstract

The utility model discloses a forming die for a space component, which relates to the technical field of processing of space components and aims to solve the problems that an existing forming die for the space component has no good heat dissipation structure, so that after the forming of the part, rapid cooling treatment cannot be performed, the forming efficiency of the part is low, and the production efficiency of the die is affected. The effects of convenient heat dissipation and stable work are achieved.

Description

Forming die for aerospace component
Technical Field
The utility model relates to the technical field of aerospace component processing, in particular to a aerospace component forming die.
Background
The aerospace component is all components and parts which are necessary under the condition of resisting the complex environment of aerospace space, because the complexity and the height of the aerospace component are required, each detail is required to be strictly controlled, the manufacturing difficulty and the cost are relatively high, the manufacturing difficulty and the cost are also one of important manifestations of the aerospace technology strength of various countries, and a forming die is required to be used for some parts with specific shapes in the aerospace component.
The prior art solutions described above have the following drawbacks: the existing forming die for the space component has no good heat dissipation structure, so that after the component is formed, quick cooling treatment cannot be performed, the efficiency of component forming is low, and the production efficiency of the die is affected.
Disclosure of Invention
The utility model aims to provide a space component forming die capable of automatically performing cooling treatment.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
the utility model provides a space component forming die, includes base and bed die, the installation cavity has been seted up to the inside of bed die, the inside fixedly connected with cooling tube in installation cavity, the one end fixedly connected with first joint in the cooling tube outside, the outside fixedly connected with first connecting pipe of first joint, the other end fixedly connected with second joint in the cooling tube outside, the outside fixedly connected with second connecting pipe of second joint, the inside fixedly connected with bin of base, be provided with the delivery pump between bin and the second connecting pipe.
Through adopting above-mentioned technical scheme, through carrying the cooling liquid in the cooling tube, from the other end of cooling tube to the storage box that flows back again, realize the circulation of cooling liquid and use, can carry out the heat dissipation to the bed die when the shaping, improve the production efficiency of mould.
Further, the inside cavity of cooling tube, the equidistant five that are provided with of cooling tube, five the inside at first joint is all installed to the one end of cooling tube, and five the other end of cooling tube is all installed in the inside of second joint, first joint and second joint are the same in size, and the specification is unanimous, switch on each other between first connecting pipe and second connecting pipe and the bin.
Through adopting above-mentioned technical scheme, install the one end of joint and five connecting pipes for can pour into the cooling liquid into five cooling tubes simultaneously, improve radiating efficiency.
Further, the inside fixedly connected with baffle of storage box, the inside of storage box is located one side fixedly connected with condensation plate of baffle, the inside of storage box is located the opposite side of baffle and is provided with the coolant liquid.
Through adopting above-mentioned technical scheme, carry out quick cooling through the cooling liquid after the cold plate to the absorption heat, make things convenient for follow-up cooling treatment to the mould.
Further, the upper end fixedly connected with support frame of base, the upper end fixedly connected with pneumatic cylinder of support frame, the flexible end fixedly connected with movable plate of pneumatic cylinder, the lower extreme fixedly connected with of movable plate goes up the mould, the outside fixedly connected with control panel of base, the inside fixedly connected with lifting unit of base, the ladder groove has been seted up to the bottom of bed die, the inside block in ladder groove has the jacking board.
Through adopting above-mentioned technical scheme, through increasing the jacking board in the bottom of bed die, can be with the part after the shaping from the inside ejection of bed die through lifting unit, conveniently get the material.
Further, the inside of lifting assembly is including fixed column, motor, lead screw, removal post and screw hole, the inside fixedly connected with motor of fixed column, the output fixedly connected with lead screw of motor, the outside of lead screw is located the inside of fixed column and is provided with the removal post, the screw hole has been seted up to the inside of removal post.
Through adopting above-mentioned technical scheme, drive the lead screw through the motor and rotate for the removal post that is located the lead screw outside removes along the screw thread, will be located the jacking plate jack-up in the removal post outside, can be with the ejecting bed die of part that is located the jacking plate upper end, realize the ejection of compact.
Further, lifting assembly symmetry is provided with two, remove post and jacking board fixed connection, it extends to the inside of ladder groove to remove the post and pass the base, it slides in the inside of fixed column to remove the post, lead screw and screw hole threaded connection, sliding connection between movable plate and the support frame, control panel and delivery pump and motor electric connection.
Through adopting above-mentioned technical scheme, through the structure of symmetrical design, when can realizing the jacking, can improve the stability of structure, convenient structure can be better use.
In summary, the beneficial technical effects of the utility model are as follows:
1. the cooling pipe is adopted, and the cooling liquid in the storage box is conveyed into the cooling pipe through the conveying pump, so that the lower die is cooled rapidly, parts in the lower die can be rapidly formed, meanwhile, the cooling liquid can flow back into the storage box again along the cooling pipe, the recycling of the cooling liquid can be realized, and the effect of convenient heat dissipation is achieved;
2. the lifting assembly and the lifting plate are adopted, the lifting plate is lifted up through the lifting assembly, so that after the part is formed, the mould can be rapidly removed, and meanwhile, the lifting assembly is stable in structure and safer to use, and the effect of stable work is achieved.
Drawings
FIG. 1 is a schematic diagram of the overall structure of the present utility model;
FIG. 2 is a schematic diagram of a heat pipe according to the present utility model;
FIG. 3 is a schematic view of the internal cross-sectional structure of the base of the present utility model;
fig. 4 is a schematic perspective view of a base of the present utility model.
In the figure, 1, a base; 2. a lower die; 3. a mounting cavity; 4. a heat radiating pipe; 5. a first joint; 6. a first connection pipe; 7. a second joint; 8. a second connection pipe; 9. a storage box; 10. a transfer pump; 11. a support frame; 12. a hydraulic cylinder; 13. a moving plate; 14. an upper die; 15. a control panel; 16. a lifting assembly; 17. a stepped groove; 18. a jacking plate; 161. fixing the column; 162. a motor; 163. a screw rod; 164. a moving column; 165. a threaded hole; 91. a partition plate; 92. a condensing plate; 93. and (5) cooling liquid.
Detailed Description
The present utility model will be described in further detail with reference to the accompanying drawings.
Referring to fig. 1-3, a space component forming die, including base 1 and bed die 2, the inside of bed die 2 has been seted up installation cavity 3, the inside fixedly connected with cooling tube 4 of installation cavity 3, the one end fixedly connected with first joint 5 in the cooling tube 4 outside, the outside fixedly connected with first connecting tube 6 of first joint 5, the other end fixedly connected with second joint 7 in the cooling tube 4 outside, the outside fixedly connected with second connecting tube 8 of second joint 7, the inside fixedly connected with bin 9 of base 1, be provided with delivery pump 10 between bin 9 and the second connecting tube 8, cooling tube 4 inside cavity, cooling tube 4 equidistant five are provided with, the inside at first joint 5 is all installed to the one end of five cooling tubes 4, the inside at second joint 7 is all installed to the other end of five cooling tubes 4, first joint 5 and second joint 7 size are the same, the specification is unanimous, all put through each other with bin 9 between the second connecting tube 8, bin 9's inside fixedly connected with baffle 91, bin 9 inside is located at one side baffle 91 and is located at the inside of bin 92, can be in order to realize that the cooling fluid is located in the cooling tube 2, the cooling fluid is in the die 93, the cooling fluid is carried out to the cooling tube is in the inside of the cooling tube is located at the die, the opposite side, the cooling fluid is cooled down in the die 93, the realization, the cooling fluid is circulated in the other side is carried out, and is cooled down in the cooling tube is cooled down the 3, and is cooled down in the cooling down condition, and is cooled down by the cooling down and is cooled down.
As shown in fig. 1-4, the upper end fixedly connected with support frame 11 of base 1, the upper end fixedly connected with pneumatic cylinder 12 of support frame 11, the telescopic end fixedly connected with movable plate 13 of pneumatic cylinder 12, the lower extreme fixedly connected with upper die 14 of movable plate 13, the outside fixedly connected with control panel 15 of base 1, the inside fixedly connected with lifting assembly 16 of base 1, step groove 17 has been seted up to the bottom of lower die 2, the inside block of step groove 17 has jacking plate 18, the inside of lifting assembly 16 includes fixed column 161, motor 162, lead screw 163, movable column 164 and screw hole 165, the inside fixedly connected with motor 162 of fixed column 161, the output fixedly connected with lead screw 163 of motor 162, the outside of lead screw 163 is located the inside of fixed column 161 and is provided with movable column 164, threaded hole 165 has been seted up to the inside of movable column 164, lifting assembly 16 symmetry is provided with two, movable column 164 and jacking plate 18 fixed connection, movable column 164 passes the inside of base 1 to step groove 17, movable column 164 slides in the inside of fixed column 161, lead screw 163 and threaded hole 165 are connected with threaded hole 165, movable plate 13 and movable plate 13 are connected with lifting assembly 15 through the inside of step groove 17, can be through the inside of step groove 17, the inside of die 2 is connected with the inside of lifting assembly 2 through the control panel 15, the inside of lift assembly 2 is formed from the bottom die 2, the inside of die 2 is connected with the bottom part through the inside of the lifting assembly 2.
The implementation principle of the embodiment is as follows: firstly, the lower die 2 and the upper die 14 are combined to start forming of parts, meanwhile, the conveying pump 10 is started to convey the cooling liquid 93 in the storage box 9 into the radiating pipe 4 to start cooling treatment of the lower die 2, meanwhile, the cooling liquid 93 flows into the first connecting pipe 6 along the radiating pipe 4, at the moment, the cooling liquid 93 flows back into the storage box 9 again to realize recycling of the cooling liquid 93, after the parts are formed, the upper die 14 is driven to be opened under the control of the hydraulic cylinder 12, the motor 162 is started at the moment, the screw rod 163 is driven to rotate through the motor 162, the moving column 164 positioned outside the screw rod 163 moves, the jacking plate 18 positioned in the stepped groove 17 is jacked, the parts positioned at the upper end of the jacking plate 18 are jacked out of the lower die 2, quick material taking is realized, the operation is convenient, and the production efficiency of the dies is improved.
The embodiments of the present utility model are all preferred embodiments of the present utility model, and are not intended to limit the scope of the present utility model in this way, therefore: all equivalent changes in structure, shape and principle of the utility model should be covered in the scope of protection of the utility model.

Claims (6)

1. The utility model provides a space flight part forming die, includes base (1) and bed die (2), its characterized in that: the inside of bed die (2) has been seted up installation cavity (3), the inside fixedly connected with cooling tube (4) of installation cavity (3), the one end fixedly connected with first joint (5) in cooling tube (4) outside, the outside fixedly connected with first connecting pipe (6) of first joint (5), the other end fixedly connected with second joint (7) in cooling tube (4) outside, the outside fixedly connected with second connecting pipe (8) of second joint (7), the inside fixedly connected with bin (9) of base (1), be provided with delivery pump (10) between bin (9) and second connecting pipe (8).
2. The aerospace component-forming die of claim 1, wherein: the inside cavity of cooling tube (4), cooling tube (4) equidistant are provided with five, and five the one end of cooling tube (4) is all installed in the inside of first joint (5), five the other end of cooling tube (4) is all installed in the inside of second joint (7), first joint (5) and second joint (7) size are the same, and the specification is unanimous, switch-on each other between first connecting pipe (6) and second connecting pipe (8) and storage box (9).
3. The aerospace component-forming die of claim 1, wherein: the inside fixedly connected with baffle (91) of storage case (9), the inside of storage case (9) is located one side fixedly connected with condensation plate (92) of baffle (91), the inside of storage case (9) is located the opposite side of baffle (91) and is provided with coolant liquid (93).
4. The aerospace component-forming die of claim 1, wherein: the utility model discloses a lifting device for a building, including base (1), support frame (11) of upper end fixedly connected with, the upper end fixedly connected with pneumatic cylinder (12) of support frame (11), the flexible end fixedly connected with movable plate (13) of pneumatic cylinder (12), the lower extreme fixedly connected with of movable plate (13) goes up mould (14), the outside fixedly connected with control panel (15) of base (1), the inside fixedly connected with lifting unit (16) of base (1), ladder groove (17) have been seted up to the bottom of bed die (2), the inside block in ladder groove (17) has jacking board (18).
5. The aerospace component-forming die of claim 4, wherein: the inside of lifting assembly (16) is including fixed column (161), motor (162), lead screw (163), removal post (164) and screw hole (165), the inside fixedly connected with motor (162) of fixed column (161), the output fixedly connected with lead screw (163) of motor (162), the outside of lead screw (163) is located the inside of fixed column (161) and is provided with removal post (164), screw hole (165) have been seted up to the inside of removal post (164).
6. The aerospace component-forming die of claim 5, wherein: lifting assembly (16) symmetry is provided with two, remove post (164) and jacking board (18) fixed connection, remove post (164) and pass the inside that base (1) extended to ladder groove (17), remove post (164) and slide in the inside of fixed column (161), lead screw (163) and screw hole (165) threaded connection, sliding connection between movable plate (13) and support frame (11), control panel (15) and delivery pump (10) and motor (162) electric connection.
CN202321178613.5U 2023-05-16 2023-05-16 Forming die for aerospace component Active CN219829205U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202321178613.5U CN219829205U (en) 2023-05-16 2023-05-16 Forming die for aerospace component

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202321178613.5U CN219829205U (en) 2023-05-16 2023-05-16 Forming die for aerospace component

Publications (1)

Publication Number Publication Date
CN219829205U true CN219829205U (en) 2023-10-13

Family

ID=88244762

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202321178613.5U Active CN219829205U (en) 2023-05-16 2023-05-16 Forming die for aerospace component

Country Status (1)

Country Link
CN (1) CN219829205U (en)

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